FIELD: space engineering.
SUBSTANCE: invention relates to testing equipment and can be used in designing space vehicle power supply systems. The proposed device incorporates load simulator, storage batteries, solar battery simulator, voltage stabilisation and automatic control complex comprising charge/discharge devices, voltage stabiliser and ACS, "plus" and "minus" busses, automatic control system with computer and lines of data exchange between ACS, load simulator and stand subsystems, auxiliary equipment, base and correcting circuits.
EFFECT: higher accuracy and reliability of power supply system simulation.
2 dwg
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